View from above orbital plane
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View from above satellite
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Ground track
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The orbit data is extracted from the following two-line orbital elements,
1 24278U 96046B 14109.13482000 .00000042 00000-0 75466-4 0 3533
2 24278 098.5156 131.1359 0351573 090.9217 313.9957 13.53020936872684
| Epoch (UTC): | 19 April 2014 03:14:08 |
| Eccentricity: | 0.0351573 |
| inclination: | 98.5156° |
| perigee height: | 799 km |
| apogee height: | 1323 km |
| right ascension of ascending node: | 131.1359° |
| argument of perigee: | 90.9217° |
| revolutions per day: | 13.53020936 |
| mean anomaly at epoch: | 313.9957° |
| orbit number at epoch: | 87268 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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